Books on the topic 'Ames and micronucleus test'

Soderman, Paul T. Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-Foot Wind Tunnel. Ames Research Center, 1990.

Soderman, Paul T. Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Fisher, David. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. National Aeronautics and Space Administration, 1996.

Fisher, David. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. National Aeronautics and Space Administration, 1996.

Test No. 474: Mammalian Erythrocyte Micronucleus Test. OECD Publishing, 1997. http://dx.doi.org/10.1787/9789264071285-en.

Test No. 474: Mammalian Erythrocyte Micronucleus Test. OECD, 2014. http://dx.doi.org/10.1787/9789264224292-en.

Test No. 474: Mammalian Erythrocyte Micronucleus Test. OECD, 2016. http://dx.doi.org/10.1787/9789264264762-en.

Test No. 487: In Vitro Mammalian Cell Micronucleus Test. OECD Publishing, 2010. http://dx.doi.org/10.1787/9789264091016-en.

Test No. 487: In Vitro Mammalian Cell Micronucleus Test. OECD Publishing, 2014. http://dx.doi.org/10.1787/9789264224438-en.

Test No. 487: In Vitro Mammalian Cell Micronucleus Test. OECD, 2016. http://dx.doi.org/10.1787/9789264264861-en.

Overview of the NASA Ames-Dryden integrated test facility. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

David, McBride, Cohen Dorothea, and Dryden Flight Research Facility, eds. Overview of the NASA Ames-Dryden integrated test facility. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1990.

Facility, Dryden Flight Research, ed. The western aeronautical test range of NASA Ames Research Center. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985.

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1989.

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1989.

Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

R, Collette J. G., and United States. National Aeronautics and Space Administration., eds. Results of a FRSI material test under Space Shuttle ascent conditions in the Ames Research Center SX7 foot supersonic wind tunnel. National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, 1992.

B, Kingsland R., Lyndon B. Johnson Space Center. Systems Engineering Division., and Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services., eds. Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310). Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.

O, Thomas Flint, Nelson Robert C, and United States. National Aeronautics and Space Administration., eds. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. National Aeronautics and Space Administration, 1996.

O, Thomas Flint, Nelson Robert C, and United States. National Aeronautics and Space Administration., eds. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. National Aeronautics and Space Administration, 1996.

Lyndon B. Johnson Space Center. Systems Engineering Division. and Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services., eds. Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42). Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.

Lyndon B. Johnson Space Center. Systems Engineering Division. and Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services., eds. Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42). Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.